glass frit as a hermetic joining layer in laser based

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Technological University Dublin Technological University Dublin ARROW@TU Dublin ARROW@TU Dublin Articles School of Electrical and Electronic Engineering 2010 Glass Frit as a Hermetic Joining Layer in Laser Based Joining of Glass Frit as a Hermetic Joining Layer in Laser Based Joining of Miniature Devices Miniature Devices Qiang wu Technological University Dublin, [email protected] Norbert Lorenz Heriot-Watt University Kevin Cannon Heriot-Watt University See next page for additional authors Follow this and additional works at: https://arrow.tudublin.ie/engscheceart Recommended Citation Recommended Citation Wu, Q. et al. (2010) Glass Frit as a Hermetic Joining Layer in Laser Based Joining of Miniature Devices, IEEE Transactions on Components and Packaging Technologies, vol. 33, no. 2, pp. 470-477. doi:10.1109/ TCAPT.2010.2045000 This Article is brought to you for free and open access by the School of Electrical and Electronic Engineering at ARROW@TU Dublin. It has been accepted for inclusion in Articles by an authorized administrator of ARROW@TU Dublin. For more information, please contact [email protected], [email protected]. This work is licensed under a Creative Commons Attribution-Noncommercial-Share Alike 4.0 License

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Technological University Dublin Technological University Dublin

ARROW@TU Dublin ARROW@TU Dublin

Articles School of Electrical and Electronic Engineering

2010

Glass Frit as a Hermetic Joining Layer in Laser Based Joining of Glass Frit as a Hermetic Joining Layer in Laser Based Joining of

Miniature Devices Miniature Devices

Qiang wu Technological University Dublin, [email protected]

Norbert Lorenz Heriot-Watt University

Kevin Cannon Heriot-Watt University

See next page for additional authors

Follow this and additional works at: https://arrow.tudublin.ie/engscheceart

Recommended Citation Recommended Citation Wu, Q. et al. (2010) Glass Frit as a Hermetic Joining Layer in Laser Based Joining of Miniature Devices, IEEE Transactions on Components and Packaging Technologies, vol. 33, no. 2, pp. 470-477. doi:10.1109/TCAPT.2010.2045000

This Article is brought to you for free and open access by the School of Electrical and Electronic Engineering at ARROW@TU Dublin. It has been accepted for inclusion in Articles by an authorized administrator of ARROW@TU Dublin. For more information, please contact [email protected], [email protected].

This work is licensed under a Creative Commons Attribution-Noncommercial-Share Alike 4.0 License

Authors Authors Qiang wu, Norbert Lorenz, Kevin Cannon, and Duncan Hand

This article is available at ARROW@TU Dublin: https://arrow.tudublin.ie/engscheceart/162

Glass frit as a hermetic joining layer in laser based joining of miniature devices

Qiang Wu1,2, Norbert Lorenz1, Kevin Cannon3 and Duncan P. Hand1

1Applied Optics and Photonics Group, School of Engineering and Physical Sciences, Heriot-Watt University EH14 4AS UK

2currently with Photonics Research Centre, School of Electronic and Communications Engineering, Dublin Institute of Technology, Kevin Street, Dublin 8, Ireland

3GE Aviation Systems, Alexandra Way, Ashchurch, Tewkesbury, Glos GL20 8TB

Abstract

In this paper we investigate the feasibility of using a laser as the heat source to drive a hermetic joining process based

on a glass frit intermediate layer. The laser allows the necessary heat energy to be provided in a localised manner;

important either as part of a multi-stage process, or to allow thermally-sensitive materials to be used inside the

package. Our study includes an investigation of the impact of rough and grooved surfaces on the hermeticity and

strength of the join, demonstrating the robust nature of the process, and its ability to allow feed-throughs to the centre

of package. Hermetic sealing is demonstrated, with leak rates of 10-9 mbar l s-1, satisfying the military standard

MIL-STD-883G.

Keywords: Laser joining, glass frit

1 Introduction

Many miniature optical, electronic and micro-mechanical systems, for example MEMS (Micro-Electro-Mechanical

Systems) require hermetic sealing with long-term stability. The dictionary definition of the term hermetic is a seal that

is completely gas tight or impermeable to gas flow. With MEMS technologies it means an air tight seal which will

keep gases and moisture out of the package; hence failure of the device due to condensing water vapour inside the

package is avoided. Appropriate bonding processes can ensure that a package remains dry and at a high vacuum for

years. As no seal is perfect standards have been defined to describe the conditions and leak rates under which seals are

still considered to be hermetic. These include the MIL-STD-883G Method 1014.11, JEDEC Standard

JESD22-A109-A and ASTM F134-85, all of which are variants of each other. A description of the leak tests according

to these standards is given in [1].

A number of different hermetic joining techniques have been developed for miniature devices, typically requiring the

whole device to be heated to a high temperature. However, this whole package heating limits the ubiquity of the

process, (i) causing problems in manufacturing processes where a number of thermal process steps are carried out in

sequence, when a later heating step can cause parts joined earlier to disassemble; and (ii) preventing the use of

temperature-sensitive materials inside the device e.g. polymers or magnetic materials. Alternative, more localised,

techniques have therefore been developed, including resistive heating [2-5]; microwave heating [6]; and induction

heating [7-8]. These require specialised modified components and/or materials; our approach is to instead use a laser

to provide this localised heating. Lasers are, of course, widely used in a range of joining processes, including the

joining of dissimilar materials such as cemented carbides to steel [9], magnesium and aluminium [10], and borosilicate

glass to fused silica [11]. These techniques create a direct bond without any intermediate layer; however they normally

require both a high temperature and highly cleaned polished contact surfaces. The use of an intermediate layer has

advantages which include a relatively low joining temperature (few hundred degrees Celcius), and less stringent

requirements for contact surface smoothness. Suitable intermediate layers include Au/Sn solder [12], Zn [13], Al, Au

[14], In [15], Ti [16], thermosetting polymer benzocyclobutene (BCB) [17], or glass frit [18-22]. Glass frits are of

particular interest due to the required low bonding temperatures ( < 595 K ), their ability to deliver a hermetic seal

with moderately rough bonding surfaces, and to conform to the surfaces being bonded - even to the extent of allowing

metallic feed-throughs to be included in the joining layer [19-20]. However current glass frit-based technologies are

based on whole-package heating in a furnace. Laser based joining should allow the advantages of glass frits to be

applied to temperature-sensitive processes and/or materials, and in multi-step manufacturing processes; however to

our knowledge there has to date been no report on laser-based joining using a glass frit intermediate layer.

Frit is simply broken particles of glass, sorted by various grind sizes, and held in a suitable binder, typically as a paste.

Sizes range from finely ground powder to small chunks. The glass frit used in our experiments is DM2700P/H848

from DIEMAT [23]. The paste comprises a low temperature glass powder loaded in an organic system which must be

burnt out completely, and the glass glazed, before joining. It can be screen-printed, stencil-printed or dispensed (e.g.

from a syringe) onto one of the surfaces to be joined; in our experiments a syringe was used to provide a layer of about

250 µm thickness once glazed. The part with deposited glass frit paste is then heated to 520 K for 30 minutes to

provide the organic burn-out before glazing for 1 minute at 620 K. The glazed surface is then mated to the other

component under slight pressure and fired at a peak temperature ranging from 593 to 648 K for as little as 1 minute to

achieve a reliable, hermetic seal.

In this paper we investigate the feasibility of this glass frit / laser process with 4 different miniature packages:

(i) LCC (Leadless chip carrier) package. This consists of an alumina-based substrate containing a recess, to

which a KovarTM lid is bonded;

(ii) planar LTCC (low temperature co-fired ceramic), an alumina-based ceramic to which a KovarTM

“top-hat” lid is bonded;

(iii) planar AlN (Aluminium Nitride) to which a KovarTM “top-hat” lid is bonded;

(iv) planar silicon substrate to which either a KovarTM or Nickel cap is bonded.

All are realistic packages used in actual device manufacture.

We first of all concentrate on the ability of the laser to provide the required localised heating, but without taking

measures to prevent heating inside the devices due to lateral conduction. We subsequently investigate the ability of

the laser/glass frit process to bond rough and grooved surfaces, and finally describe a process whereby the temperature

inside the device is minimised by the use of appropriate heat-sinking, including both experimental and simulation

results.

2 The laser-glass frit joining process

The laser used is a fibre-delivered diode array operating at 940 nm (Laserline, fibre core diameter 200 µm, NA=0.22).

A galvanometer scanner was used together with an f-theta lens to provide a focused spot of diameter 1 mm which

could be moved at high speed across the workpiece. Alternatively, an axicon lens could be used together with a

conventional lens to generate a ring focus, as described in section 4.3 below. A schematic of the laser bonding

arrangement is shown in Figure 1(b).

(a) (b)

Figure 1 (a) experimental setup and (b) schematic of laser bonding with scanned laser beam

2.1. Laser bonding of LCC (Leadless Chip Carrier) packages

The LCC substrate is made from a high temperature co-fired ceramic, made by companies such as Kyocera and NTK.

The ceramic is mostly (90%) alumina (Al2O3), with some other glassy materials for binding. The dimensions of the

Kovar™ lid and LCC substrate are 12.7 × 12.7 mm and 13.7 × 13.7 mm respectively. The substrate includes a recess

8.9 × 8.9 mm by 1.27 mm deep. Figure 2 shows (a) the LCC substrate and (b) the Kovar™ lid (syringe-dispersed

glass frit followed by organic burn-out and glazing with thickness around 250 µm) before bonding and (c) the bonded

sample. In this case, to improve the laser beam absorption, a piece of silicon wafer of thickness 380 µm was placed in

good thermal contact with the Kovar™ lid as shown in the figure, absorbing 69% of the 940 nm laser light.

Figure 2 (a) LCC substrate and (b) Kovar™ lid (dispersed with glass frit) before bonding and (c) bonded sample

Fine and gross leak tests were carried out for the bonded samples, using a two-part process [1]; the gross leak test is

essentially a pass/fail; whilst the fine leak test results are shown in table 1. The acceptable leak rate, as defined by

(a) (b) (c)

MIL-STD-883G, is 5 × 10-8 mbar l s-1 for a package of this volume. It is clear from the results presented in the table

that a lower rate than this was achieved for a range of laser powers and bonding times.

Table 1 Fine leak test results of bonded LCC packages

Laser Power (W) Force (N) Bonding time (s) Leak rate (mbar l s-1)

35 2.25 140 1.3 × 10-9

40 1.96 100 1.1 × 10-9

60 1.96 40 2.2 × 10-9

Sectioning and polishing of the bonded sample were carried out to visually assess the joint quality across the bond. A

typical micrograph of a sectioned sample is shown in figure 3, which indicates that glass frit has excellent contact with

both the LCC substrate and KovarTM lid, with no visible voids; it appears to have conformed well to the locally rough

ceramic surface.

Figure 3 Micrograph of sectioned LCC package

2.2. Laser bonding of Top-hat packages

The “top-hat” cap consists of a raised square cap made of Kovar™, coated with a thin layer of nickel and then gold;

however there was no coating at the bonding area – see figure 4(a) and (b). This cap is 9 × 9 mm, and 4 mm high. Two

kinds of substrates were used in our experiments: AlN, 13 × 13 × 0.5 mm (figure 4(c)), whilst the other is LTCC,

18 × 18 × 0.6 mm (figure 4(d)). The LTCC was plated with a 10μm thick Au track in the bonding region.

(a)

(b)

(c)

(d)

Figure 4 (a) Sketch of “top-hat” cap; (b) “top-hat” Kovar™ cap dispersed with glass frit; (c) AlN and (d) LTCC substrate

In this case joining was carried out with the samples inverted; i.e. with the substrate uppermost. Examples of the

bonded samples are shown in figure 5.

(a) (b)

Figure 5 Laser bonded sample of (a) AlN and (b) LTCC substrate to top-hat cap

Successful bonding was achieved, although a higher power laser power of ∼ 100W was required for LTCC, in

comparison with 40 - 50 W with AlN. These bonded samples all passed the gross leak test, and met the MIL-STD

883G criteria in the fine leak test (again 5 × 10-8 mbar l s-1, given the 0.26 cm3 internal volume). Detailed results are

shown in tables 2 and 3 below. The bonding force used in each case was 1.96 N.

Table 2 Fine leak test results of AlN substrate bonded to top-hat Kovar™ cap

Laser Power (W) Bonding time (s) Leak rate (mbar l s-1)

40 40 4.8 × 10-9

45 30 1.1 × 10-9

50 26 1.3 × 10-9

Table 3 Fine leak test results of LTCC substrate bonded to top-hat Kovar™ cap

Laser Power (W) Bonding time (s) Leak rate (mbar l s-1)

100 80 1.4 × 10-9

120 50 1.7 × 10-9

To visually assess the bonded joint, samples were sectioned and polished. Example micrographs are shown in

figure 6. Again, the glass frit makes excellent contact with both these samples, conforming well to the joined surfaces.

(a) (b)

Figure 6 Micrograph of section (a) AlN and (b) LTCC substrate to top-hat Kovar™ cap

3 Influence of micro-machined channels/slots on hermeticity and shear force

Bonding surface roughness is an important issue in most hermetic packaging technology. Many processes require

very flat surfaces to be used; however the results presented above demonstrate that the glass frit has the ability to

conform well to naturally rough surfaces. In this section we report on our more detailed investigation of the impact of

non-planar joining surfaces on hermeticity and shear strengths; specifically surfaces containing micro-machined

channels / slots.

In this section we introduce our final sample, which has a silicon substrate, in addition to the LTCC and AlN substrates

used in the experiments described earlier. Each substrate was modified by laser machining a series of closely-spaced

slots into the surface. The slot depth generated was slightly different in each case, as shown in the micrographs of

sectioned samples in figure 7; meanwhile the SEM images shown in figure 8 provide an indication of the extent the

surface roughness in each case. The slot depths are shown more clearly in the micrographs shown in figure 8.

(a) (b) (c)

Figure 7 Micrographs of the cross-section of laser machined (a) LCC (b) AlN and (c) silicon substrate

(a) (b)

(c)

Figure 8 SEM images of the surface roughness of laser machined substrates (a) LCC (b) AlN and (c) silicon, providing an indication of surface roughness, both of the original sample and in the laser-machined region

Of interest here is not only the leak rate that can be achieved, but also the shear strength. First of all, non-machined

samples were tested. The LCC packages had a shear strength of 62 kg, whilst both the AlN and silicon were only

∼ 5 kg. With the laser-machined samples, leak rates of less than 5 × 10-8 mbar l s-1 were consistently achieved,

demonstrating the excellent ability of the glass frit to conform to the joining surfaces. The laser machining did,

however, influence the shear strength for both the AlN and silicon substrates; in both cases it was increased to ∼ 10 kg

provided that the grooves were at least 20 – 30 µm deep. With the LCC substrate, no such increase was observed;

however it is clear from figure 8 that the unprocessed surface in this case already has a significant roughness in

comparison with the other samples. It is hence clear that one potential drawback of glass frit is a relative lack of

strength when joining very smooth surfaces; however in general it is easier to produce a sample with rough surface

than a smooth one.

To visually assess the joint line of bonded area, sectioning and polishing of the bonded samples were carried out.

Micrographs of the sectioned samples are shown in figure 9; here it is clear that the glass frit has flowed into the

laser-machined slot, providing excellent contact in all cases.

(a) (b) (c)

Figure 9 Micrographs of sectioned packages, (a) LCC with a KovarTM lid; (b) AlN with KovarTM “top-hat” cap and (c) silicon with KovarTM “top-hat” cap

4 Laser based localised bonding technique

In the investigations detailed above, we were not concerned about preventing heating inside the joined packages;

indeed for simplicity the samples to be joined are placed on top of a glass slide. However this will heat the whole

sample to a high temperature due to the lateral heat transfer, in particular with the silicon substrate, which has a high

thermal conductance. To prevent lateral heating of the centre of the substrate, it is necessary to place a cooled

thermally conductive block (in our case copper was used) in contact with the underside of the substrate, to act as a heat

sink [24]. To prevent excessive heat loss, and hence reduce the requirement for average laser power, this heat sink was

designed to be only in contact with the centre of the package, to cool any temperature-sensitive elements inside, as

shown in figure 10.

Figure 10 schematic of localised laser bonding with copper boss cooling unit

To test this cooling technique, we investigated the bonding of a TO5 Nickel cap to silicon; this particular sample was

chosen as in this case truly localised heating is particularly difficult to achieve, given the high thermal conductivity of

the silicon substrate. It is important to ensure a uniform temperature throughout the glass frit, to ensure that it is fully

cured. As a result the approach adopted for laser heating was to scan the focused laser spot on the silicon substrate,

just outside the Ni cap, in a ring of diameter 10.4 mm and width 0.35 mm.

4.1 Finite element simulation

In addition to the experiments, a finite element simulation was constructed in FlexPDE to determine the temperature

field likely to be generated in this case. The simulation is based on the heat equation in an isotropic and homogeneous

medium:

)( 2

2

2

2

2

2

zu

yu

xu

ctu

∂∂

+∂∂

+∂∂

=∂∂

ρκ (1)

where u=u(t,x,y,z) is temperature which is a function of both time and space; κ is the thermal conductivity; c is the specific heat, and ρ the density.

We assumed that the laser heat source has a Gaussian Irradiance profile

)2exp()1(2)( 2

2

2 ωπωrRPrI −−= (2)

Where P is the laser output power, R is the reflectivity of material, ω is the radius of the laser beam.

This model was constructed for the setup shown in figure 10 and the laser energy was assumed to be absorbed at the

surface of the silicon (of thickness 380 µm and reflectivity of 31%). The temperature at the bottom surface of the

copper is fixed at 300 K (water cooled), and the temperature at the top layer of glass is also assumed as 300 K and the

heat transfer coefficient of ambient air is 40 W m-2 K-1 [25]. Radiative heat transfer was also included between the

closely spaced surfaces in the device and into the surrounding air. To simplify the simulation process, we assume first

of all that the temperature has reached a steady state and the laser illumination on the silicon surface is continuous

because of its very high scanning speed (1000 mm/s), forming a ring of diameter 10.4 mm and width 0.35 mm.

However, a time-dependant simulation was also carried out to investigate the evolution of temperature with time.

Results from this model are presented in figure 11(c), for 3 points on the silicon surface, namely in the centre of the

silicon chip, within the glass frit ring and directly below the laser illumination track.

We also assume an imperfect thermal contact between the copper boss and silicon, as they are not completely flat, but

each have a certain surface roughness; to model this we treat it as a 3 µm air gap. The outer diameter of the TO5 cap is

8.3 mm and it has a ‘lip’ of width 0.5 mm at the base, whilst the substrate is 12 × 12 mm, i.e. the laser illuminates a ring

on the substrate slightly larger than the TO5 cap. Figure 11(a-b) shows the calculated temperature field arising from 61

W laser illumination.

(a)

(b)

(c)

Figure 11 Calculated temperature field (a) at the silicon substrate surface and (b) at a cross-section through the centre

of the top-hat (at y = 6 mm); (the z-axis is magnified in the figure); and (c) the temporal evolution of temperature at 3

points on the silicon surface, namely in the centre of the silicon chip, within the glass frit ring and directly below the

laser illumination track.

It can be seen in figure 11(a) that the temperature distribution expected within the glass frit ring is reasonably uniform.

The calculated temperatures at the outer and inner edges of the glass frit ring at the silicon surface are 664 K and 626

K respectively, a difference of 38 K. Furthermore, figure 11(b) shows that the predicted temperatures on the bottom

and top of the glass frit at ring centre are 644 K and 590 K respectively, i.e. a difference of 54 K. Meanwhile, the

temperature at the centre of the silicon substrate should be kept to around 420 K, so the heating is properly localised.

It can be seen from figure 11(c) that after 10 s laser illumination, the temperatures in the centre of the silicon chip,

within the glass frit ring and directly below the laser illumination track are 724, 634 and 418 K respectively; in each

case this is at least 97% of the temperature at steady state. This indicates that the steady state model is appropriate for

the laser scanning times used here.

It is noted that it is important to include the effect of radiative heat transfer in the model; if this is omitted, the

simulated maximum temperature obtained with a reduced laser power of 58W is the same as that with a laser power

61W when radiation is included.

4.2 Experimental – scanning beam

A series of experiments were carried out; however there was found to be a problem on the cooling phase. A few

seconds after completing the laser heating phase, a ‘cracking’ noise could always be heard. On inspection it was clear

that a thermally-induced crack was occurring in the glass frit. Such a crack is likely to arise from different cooling

rates in the silicon and glass frit, due to the high thermal conductivity of both the silicon substrate and Cu support/heat

sink. It was found that reducing the laser power in a stepwise fashion, and adding a cooling gas flow to the cap

towards the end of the heating process, could reduce the likelihood of this cracking, but not completely eliminate it.

An additional refinement was therefore made to the experimental arrangement, whereby the Cu support was moved

away from the silicon substrate immediately after the laser shutter was closed, i.e. at the end of the heating cycle,

whilst the cooling gas flow was maintained for a further 15 s. After optimisation of the bonding parameters, a series of

6 samples was bonded, and an improved success rate of 66% (4 out of 6) was obtained. Parameters used were: laser

power of 55 W for 150 s, followed by 46 W for 10 s, and the cooling gas flow started at 135 s. Provided no cracking

occurred, the leak rate was always less than 2.0 × 10-9 mbar l s-1. The laser was scanned over a ring of diameter

10.4 mm, on a 12 × 12 mm silicon substrate.

To determine the maximum temperature reached in the centre of the silicon sample, further experiments were carried

out by coating the centre of the silicon with a temperature indicating paint (Tempilaq, Tempil Inc). With an

illumination laser power of 56 W for 150 seconds, this paint demonstrates that the temperature in the centre of the

silicon was in the range 505 to 526 K, higher than indicated from the simulation (most likely due to poor thermal

contact between the silicon and the copper), but still significantly below the glass frit curing temperature of around

640 K.

4.3 Experimental - focused ring

An axicon is a cone-shaped optic, and in combination with a positive lens can create a ‘ring focus’. Figure 12 shows a

cross-section through an axicon-lens arrangement, demonstrating this effect, given the circular symmetry of the

axicon.

Figure 12 Schematic figure of an axicon ring

In our setup, fibre-delivered light is collimated with a +100 mm focal length lens before passing through the axicon

followed by a positive focal length focusing lens, generating a focused laser ring of diameter 12 mm and width 1 mm.

The silicon substrate in this case was 14 × 14 mm, and as with the scanning system, the Ni cap is not heated directly,

but rather the silicon substrate immediately surrounding the cap. As with the laser scanning technique, a cooling gas

flow was used towards the end of the heating phase, and the silicon separated from the Cu cooling block at the end of

the heating phase. An illumination laser power in the range of 60 to 68 W was used for 100 s, and then reduced to

45 W for 10 s. A cooling gas flow was started 85 s after the start of the heating phase. In all cases, the parts were

successfully joined (20 parts), with a leak rate of 1.7 × 10-9 mbar l s-1 or less. Measurements with Tempilaq paint

demonstrate that the maximum temperature was in the range 505 to 526 K.

5 Conclusions and discussions

Knechtel [20] states that the advantages of glass frit bonding are high bonding strength and process yield, low stress at

the bonding interface, good process repeatability, hermetic sealing and non-stringent requirements for the flatness of

α

β

β

θ

D

f

the surfaces to be bonded. The laser-based process investigated in this paper combines these advantages with

localised heating and a high speed process.

In this paper, we have demonstrated the versatility of laser-based bonding using glass frit for a range of miniature

packages and materials, where hermetic seals are required. We have demonstrated that the process is highly suited to

rough or non-flat surfaces; indeed with a smooth surface it is beneficial to machine micro-slots into the surface before

joining. Care must however be taken when using localised heating to join materials of differing thermal parameters;

differential cooling can lead to stress across the join and hence failure by cracking of the glass frit. A potential solution

has been demonstrated in this paper for a particular sample configuration.

Acknowledgments

The authors acknowledge the financial support of the Engineering and Physical Sciences Research Council in the UK.

The authors are also grateful to Steve Riches (GE Aviation Systems), John Betterton (QinetiQ), John Gillham

(QinetiQ) for fruitful discussions and provision of samples.

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[25] http://www.cheresources.com/insulationzz.shtml

Qiang Wu received his B.S. degree from Beijing Normal University, China, in 1996 and a Ph.D degree from Beijing University of Posts and Telecommunications, China, in 2004.

From 1996 to 1999, he worked as an Assistant Lecturer in theoretical physics at Jiangxi Normal University, China. In 2004, he worked as a Senior Research Associate in the Optoelectronics Research Centre, City University of Hong Kong, carrying out research into polymer optical waveguides. From 2006 to 2008, he was a Research Associate in the Applied Optics and Photonics Group at Heriot-Watt University in Edinburgh in Scotland, research aspects of laser jointing in micro-manufacture.

Dr. Wu joined the Dublin Institute of Technology (DIT) in August 2008 as an SFI funded “Stokes Lecturer” at the School of Electronic and Communications Engineering. He is now working within the Photonics Research Group at DIT on aspects of fast optical wavelength measurement, fibre optic sensing and multi-channel fibre Bragg gratings.

Norbert Lorenz received a Diplom Ingenieur (FH) in Photonics from the University of Applied Science Emden, Germany in 2007. For the corresponding thesis he worked at the Forschungszentrum Karlsruhe, Germany, where his research aimed at the production of waveguides structures in PMMA using excimer lasers in direct writing processes. He is studying towards a PhD on the subject “Laser-joining in Microsystems” at Heriot-Watt University in Edinburgh, UK. His research concentrates on the development of new laser-based MEMS and micro-devices encapsulation processes using localised heating.

Mr K M Cannon, Bishops Stortford, Hertfordshire 1961 received a BEng degree in Electrical and Electronic Engineering from the University of Brighton, UK, in 1987.

He moved to GE Aviation, Tewkesbury (formerly Smiths Aerospace) as a Manufacturing Process Engineer in 1988 to

develop the interconnection and packaging technologies for Multi-Chip-Modules devices and participated in the RISH and MCMC funded programs.

In 2008 he was promoted to the position of Operations Manager for the site were his current interest are in the packaging of Micro System devices which includes MEM’s and Sensors technologies.

Prof Duncan Hand received a BSc degree in physics with electronics in 1986 from the University of St Andrews, UK, and a PhD entitled ‘periodic structures in optical fibres’ from the University of Southampton, UK, in 1991.

He moved to Heriot-Watt University in 1991, to work as a Research Associate. In 1997 he obtained a Lectureship position at the same institution, was promoted to Reader in 2001 and Professor of Applied Photonics in 2003. His current research interests encompass a wide range of applications of high power lasers, primarily in manufacturing processes (laser precision machining; laser joining) and in medicine (surgery; dentistry). This work includes research into the delivery of the high peak power laser light via novel optical fibres and other optics.

Prof. Hand is a Fellow of the Institute of Physics, and Consultant Professor of Beijing University of Posts and Telecommunications.